The influence of the blade feather constructional inhomogeneity on the turbine cooling blades stress-strain state

The problem of gas turbine engines inhomogeneous rotor blades stress-strain state has been studied. For this purpose, the new, more correct mathematical model, based on the special three-dimensional curvilinear finite elements has been used. Such elements have three modifications, applied for the bl...

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Bibliographic Details
Main Author: Serhii Morhun
Format: Article
Language:English
Published: PC Technology Center 2018-03-01
Series:Eastern-European Journal of Enterprise Technologies
Subjects:
Online Access:http://journals.uran.ua/eejet/article/view/125937